The role of heat conduction in leading edge heating theory and experiment /

High-speed flight propulsion systems /
Published: (1991)

Camber effects on the non-linear lift of slender wings with sharp leading edges /
by: Squire, Leonard Charles
Published: (1967)

Combined flexure and torsion of a class of heated thin wings : a large-deflection analysis /
by: Mansfield, Eric Harold, 1923-
Published: (1961)

Experimental investigation of the effect of trailing-edge sweepback on the subsonic longitudinal characteristics of slender wings, by D. L. I. Kirkpatrick and A. G. Hepworth.
by: Kirkpatrick, David L. I.
Published: (1970)

Numerical solutions of hypersonic near-wake flow by the particle-in cell method /
by: Crane, Robert Ian
Published: (1970)

Aerodynamic heating in supersonic and hypersonic flows advanced techniques for drag and aero-heating reduction /
by: Gerdroodbary, Mostafa Barzegar
Published: (2022)

Super- and hypersonic aerodynamics and heat transfer /
Published: (1993)

Supersonic flutter derivatives for a series of swept and cropped delta wings /
by: Harris, G. Z.
Published: (1967)

The pressure distribution at zero lift on a slender delta wing at transonic speeds /
by: Firmin, Michael Charles Peter, 1929-
Published: (1968)

Comparison of seven wing buffet boundaries measured in wind tunnels and in flight /
by: Mabey, Dennis G.
Published: (1966)

Measurements of buffeting on slender wing models /
by: Mabey, Dennis G.
Published: (1967)

Investigation of the normal force characteristics of slender delta wings with various rhombic cross-sections in subsonic conical flow /
by: Kirkpatrick, David L. I.
Published: (1967)

Approximate formulae for the lift and drag of wedge aerofoil sections at high supersonic speeds /
by: Squire, Leonard Charles
Published: (1966)

Developments in high-speed-vehicle propusion systems /
Published: (1996)

Low-speed wind-tunnel tests on a delta-wing aircraft model (S.R. 177) with blowing over the trailing-edge flaps and ailerons /
by: Butler, S. F. J.
Published: (1966)

Measurements of pressure distribution and shock-wave shape on power-law bodies at a mach number of 6.85 /
by: Peckham, D. H.
Published: (1967)

The derivation of power spectra of density variations in hypersonic wakes from Schlieren photographs /
by: Thompson, James Perry
Published: (1968)

Balance measurements (excluding drag) on a delta wing aircraft at transonic speeds /
by: Shaw, M. M.
Published: (1967)

The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)

Low-speed wind-tunnel measurements of the lift, drag and pitching moment on three symmetrical ogee-wing models and on a symmetrical slender wing-body model /
by: Kirby, D. A. (Donald Allen), 1926-
Published: (1966)

The drag of infite [as printed] swept wings : with an addendum /
by: Cooke, J. C. (John Caister)
Published: (1969)

Selected aerothermodynamic design problems of hypersonic flight vehicles /
by: Hirschel, Ernst-Heinrich
Published: (2009)

Non-linear theory of steady forces on wings with leading-edge flow separation /
by: Garner, Henry Clifford
Published: (1964)

Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8 /
by: Winter, Kenneth George
Published: (1968)

Morphing aerospace vehicles and structures /
Published: (2012)

Pressure distribution on two wings with curved leading edges at supersonic speeds /
by: Narayan, K. Yegna
Published: (1974)

Wind tunnel investigation of jet interference for underwing installation of high bypass ratio engines /
by: Raney, Derek John
Published: (1969)

An experimental investigation of the structure of a leading-edge vortex /
by: Earnshaw, P. B.
Published: (1962)

Measurements of wing buffeting on a Scimitar model /
by: Mabey, Dennis G.
Published: (1967)

The effect of temperature variations in the plane and through the thickness of a circular lenticular plate /
by: Mansfield, Eric Harold, 1923-
Published: (1962)

On the hypersonic leading-edge problem in the merged-layer regime /
Published: (1968)

An investigation of laminar heat transfer to slender cones in the hypersonic shock tunnel /
by: Wittliff, Charles E.
Published: (1961)

Exploratory investigation of the effects of blowing from the leading edge of a delta wing /
by: Trebble, W. J. G.
Published: (1968)

Measurements of drag, base pressure and base aerodynamic heat transfer appropriate to 8.5 semi-angle sharp cones in free flight at mach numbers from 0.8 to 3.8 /
by: Greenwood, G. H.
Published: (1967)

Thermophysical aspects of re-entry flows /
Published: (1986)

A study of the effect of leading-edge modifications on the flow over a 50-deg sweptback wing at transonic speeds /
by: Rogers, E. W. E.
Published: (1962)